Research on adaptive backstepping sliding mode control method for a hex-rotor Unmanned Aerial Vehicle

Zhuo Zhang, Zhenghua Liu, Nuan Wen
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引用次数: 5

Abstract

This paper concentrates on attitude control and spot hover about the hex-rotor Unmanned Aerial Vehicle (UAV). First of all, according to the Newton - Euler equation, set up the equations of motion in inertial frame. Then based on the characteristics of the hex-rotor UAV model, adaptive backstepping sliding mode controllers are designed to realize the attitude and position control. Finally, the control strategy is verified by the simulation. It's proved that the control system has strong robustness to both the disturbance and the parametric variation.
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六旋翼无人机自适应反步滑模控制方法研究
本文主要研究了六旋翼无人机的姿态控制和定点悬停问题。首先,根据牛顿-欧拉方程,建立了惯性系中的运动方程。然后根据六旋翼无人机模型的特点,设计了自适应反步滑模控制器来实现姿态和位置控制。最后,通过仿真验证了控制策略的正确性。结果表明,该控制系统对扰动和参数变化都具有较强的鲁棒性。
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